In 1937,
Canadian Car and Foundry obtained rights to the
Wallace Trainer designed by Leland Stamford Wallace. The nearly-complete project was a biplane with two open cockpits, powered by a
Kinner B-5 engine. Featuring welded steel-tube fuselage, ailerons and tail with a wing structure utilizing spruce spars and ribs, the aircraft was fabric covered, except for
aluminium panelled cockpit and engine areas. Canadian Car and Foundry renamed it the
Maple Leaf I. In 1938, once the Maple Leaf I was complete, the new Chief Designer Elsie McGill began work on the
Maple Leaf II, which, except for the use of the fin and rudder from the earlier aircraft, was a new design. A conventional structure based on welded steel tube fuselage and steel-tube tail, aluminium alloy ribs with wooden wings was employed. Designed around British design requirements for strength, the Maple Leaf II was intended to be fully aerobatic. In order to expedite development and to ensure no interruption in the ongoing
Hawker Hurricane production lines, a number of components were "farmed out" to sub-contractors. ==Operational history==